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WO/2021/055403A1 |
A drone-based delivery system includes a drone (200) that delivers an item (210), and a landing station (100) for landing said drone. The landing station includes a retractable receiving box (160) and a storage compartment (150) to recei...
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WO/2021/051243A1 |
A method for installing an air inlet duct protective cover of an aircraft engine, comprising the following steps: a. inflating a protective fabric cover; b. the protective cover supporting a certain prefabricated outer shape to achieve t...
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WO/2021/053875A1 |
This flying device 1 comprises: an electric power acquisition unit 12 which receives supply of electric power from a prescribed mobile body 2; a flight control unit 171 which causes the flying device 1 to fly within a prescribed range wi...
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WO/2021/055223A1 |
A modular floor system with an integral utility for temporary installation in an unfinished ircraft fuselage to facilitate construction. The system includes multiple floor modules, each ncluding a catch pan defining a pan volume, a grid ...
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WO/2021/055402A1 |
A portable landing pad (100) for landing of a drone (200) includes a platform (105) having a flat surface for receiving the drone, and multiple global positioning system (GPS) guided lasers (125) positioned at near edges of the platform ...
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WO/2021/054782A1 |
An unmanned aerial vehicle for performing a diagnostic flight before executing a flight, according to various embodiments, comprises: a flight body; a sensor module comprising a plurality of sensors; a communication module for wirelessly...
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WO/2021/053227A1 |
The invention relates to an air conditioning unit (1) for an aircraft, comprising an air circuit (10) with an air inlet (110) and an air outlet (120), at least one "positive" closed-loop cooling circuit (20), comprising a heat exchanger ...
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WO/2021/049155A1 |
The present invention strictly manages the number of aircraft that fly on a predetermined flight path in the same time slot. An operation management system 1 comprises: a flight permission determination unit 12 that, by referencing a d...
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WO/2021/048497A1 |
The present invention relates to a system (1) for recharging an unmanned aerial vehicle, comprising: - a base (20), - a supplying boom (21) comprising a tip (23) and first recharging means (24), - a receiving basket (12) comprising an in...
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WO/2021/049734A1 |
Disclosed are a sterilization device capable of sterilizing an object using plasma and ultraviolet rays, and an airport sterilization system comprising same. The sterilization device may comprise: a first sterilization unit for irradiati...
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WO/2021/046558A1 |
A cargo aircraft configured to carry a portion of its payload in a cargo bay volume enclosed by a moveable nose door and supported by a structural extension of the fuselage that extends forward into the moveable nose door is disclosed. E...
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WO/2021/043524A1 |
The invention relates to a method for charging a drone by means of a centring and charging device provided with protruding electromechanical charging contacts for rapid and high-power charging of the drone (between 500 and 1,500 watts). ...
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WO/2021/046557A1 |
Systems and methods for loading a cargo aircraft are described. The system includes at least one rail disposed in an interior cargo bay of a cargo aircraft that extends at an angle relative to an interior bottom contact surface of a forw...
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WO/2021/046559A1 |
Systems, methods, and aircraft for managing center of gravity (CG) while transporting large cargo are described. Management of CG is achieved in many ways. In some instances, the aircraft itself is designed to assist in managing CG by pr...
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WO/2021/045064A1 |
[Problem] To adapt to changes in conditions that can occur while a mobile terminal is mid-flight following a flight path and land the mobile terminal at a suitable landing position. [Solution] A control system 100 comprises: an informati...
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WO/2021/046555A1 |
Systems, methods, and vehicles for loading and unloading cargo from a long-distance transport vehicle, such as an aircraft, are described. The systems and methods include operating a plurality of vehicles to unload large cargo from the a...
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WO/2021/046545A1 |
A device is disclosed. The device includes an exterior conveyor and a storage area. The exterior conveyor is configured to convey baggage to and from the storage area. The baggage may be sorted to the storage area by a lateral sorter and...
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WO/2021/046560A1 |
A fixed-wing cargo aircraft having a kinked fuselage to extend the useable length of a continuous interior cargo bay while still meeting a tailstrike requirement is disclosed, The fuselage defines a continuous interior cargo bay along a ...
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WO/2021/039245A1 |
This distribution device (10) is provided with an acquisition unit (11) which acquires position information about an obstacle, and a distribution unit (12) which wirelessly distributes, from the obstacle to an aircraft, obstacle informat...
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WO/2021/037463A1 |
A method for autonomous in-flight transfer of a load from a first Aerial Vehicle, AV, to a second AV is provided. Each of the first AV and the second AV includes a frame with a vertical opening for receiving the load. A plurality of roto...
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WO/2021/039469A1 |
A control device (19) controls an electric drive system (10) including a drive motor (12) which is mounted in an electric vertical takeoff and landing aircraft (100) having a rotor blade (30) and which rotationally drives the rotor blade...
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WO/2021/038667A1 |
[Problem] To provide a device for controlling an unmanned aerial vehicle with which it is possible to easily implement transportation of supplies by the UAV, even at a landing site that is not equipped with a specific platform. [Solution...
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WO/2021/038302A1 |
The invention relates to a method for producing a torsion box for a structure of an aeroplane. Said method comprises the following steps: providing a first component made of a fibre composite material, which first component has a first p...
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WO/2021/037743A1 |
An energy absorbing system for arresting a vehicle (1) comprising a concrete subbase (2) positioned on a frangible support (3) and being covered with at least one polyurethane layer (4) and at least one polyurea layer (5) and a method fo...
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WO/2021/038854A1 |
A control device (200) is provided with: a traveling body control unit (230) for causing a traveling body to travel in a target area; an acquisition unit (210) for acquiring state information indicating the state of a surface on the targ...
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WO/2021/039502A1 |
Provided is an operation confirmation device (70) for an electrical driving system (10) that is mounted on an electrical vertical take-off and landing aircraft (100). The electrical driving system includes a motor for driving a rotor of ...
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WO/2021/039381A1 |
An electric vertical takeoff and landing aircraft (100, 100a - d), which includes a plurality of electric drive systems (10, 10a - d), each having a drive motor 12 that rotationally drives a rotor blade (30) and a drive unit 11 that driv...
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WO/2021/036477A1 |
A ground test bench for an aircraft oxygen system, comprising a box body (1) and a box cover (2) hinged to the box body (1). One side surface wall of the box body (1) is communicated with an air inlet tube (5) and an air outlet tube (6);...
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WO/2021/032428A1 |
Disclosed is a method for producing a structural component (2), in particular for an aircraft, ground vehicle, or watercraft, or for a rotor blade of a wind turbine, in which method an arrangement (6) consisting of fibres and a plastics ...
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WO/2021/032921A1 |
The invention concerns an apparatus for inspecting luggage, comprising a tubular frame having a plurality of pairs of lateral openings (64, 66), the tubular frame being suitable for receiving a plurality of containers (24) in line with t...
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WO/2021/033168A1 |
A method for sheltering a balloon, a blimp, or airship. The method includes obtaining a first guideway by detachably attaching a first plurality of detachable rings to a first side of an outer surface of the balloon, placing a first rope...
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WO/2021/031129A1 |
Provided are a relay communication device, an unmanned aerial vehicle hangar, a control system and a relay communication method. The relay communication device comprises: a first antenna (1), a second antenna (2) and a radio receiver (3)...
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WO/2021/034835A1 |
Aspects of the disclosure relate to envelopes for aerial vehicle. The aerial vehicle 200 may include an envelope 210 including a plurality of gores 210A, 210B. The aerial vehicle may also include a seal 230, 232 arranged between a pair o...
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WO/2021/028306A1 |
In summary, the present application relates to an aircraft interior paneling (10) comprising: - a planar replaceable surface element (40); - a structural element (20); - at least one connection element (30); wherein the replaceable surfa...
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WO/2021/029233A1 |
[Problem] To provide an aerial vehicle takeoff and landing system, a takeoff and landing apparatus for an aerial vehicle, and an aerial vehicle capable of reducing the influence of ground effect and capable of taking off and landing smoo...
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WO/2021/027888A1 |
A method for preventing a boarding bridge from colliding with a wing, comprising: establishing, in a first coordinate system, an outer contour model of a boarding bridge and an anti-collision line model, the anti-collision line model bei...
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WO/2021/022122A1 |
A control system is configured to facilitate transfer of a package between a room in a building and a delivery service outside the room associated with a shipment order. The system controls a shiftable panel of the building to selectivel...
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WO/2021/020660A1 |
A ground station for supporting a tethered drone, and a tethered drone system comprising same, according to an embodiment of the present invention, comprise: a power supply unit for supplying power to a tethered drone through a cable; a ...
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WO/2021/015201A1 |
The present invention addresses the problem of controlling a distant mobile body with high accuracy. The problem is solved by a remote piloting system and a piloting device therefor. The remote piloting system is provided with a mobile...
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WO/2021/012476A1 |
A method for controlling loading of an airport catering truck, comprising: when a power battery drives loading work, driven supporting legs to be supported only when the state of the whole truck satisfies the conditions of the normal wor...
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WO/2021/014514A1 |
This aircraft inspection assistance device (100) comprises: a three-dimensional model generating part (25a); an inspection position acquiring part (25b); and a control part (25) that acquires inspection results (50) of an inspection obje...
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WO/2021/012473A1 |
An electric aviation food vehicle, a loaded refrigeration system is provided with two power supply modes, namely a vehicle-mounted power supply and an external power supply. When the whole vehicle is in the charging state, the whole vehi...
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WO/2021/012475A1 |
A temperature control method for a refrigerated container. The staff can adjust the target temperature of an air conditioner to within a first temperature range, and an air conditioner controller can also automatically adjust the tempera...
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WO/2021/012474A1 |
A vehicle control system and control method for an electric airline catering truck. The system comprises a CAN bus network, a charging control module, a driving control module, a brake control module, a power-on/power-off mode control mo...
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WO/2021/014277A1 |
Methods for making structural shims (220) for the mating assembly of parts, such as for installation between a skin (212) and substructure (214) of an aircraft. The methods include the steps of disposing a hardenable composition (216) in...
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WO/2021/014747A1 |
[Problem] To provide an information processing device, an information processing method, and a program that, in order to avoid conflicts between mobile bodies, are configured so that some aircraft are not delayed excessively, to the exte...
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WO/2021/014134A2 |
A hydrogen storage device (100A) comprises: a pressure vessel (230A), having a first fluid inlet (210A) and/or a first fluid outlet (220A), having therein a thermally conducting network (240A) optionally thermally coupled to a first heat...
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WO/2021/014396A1 |
The present disclosure discloses an arm mechanism (100) for docking an unmanned aerial vehicle (200), to a structure for conducting non-destructive testing. The arm mechanism (100) comprises a bracket (101), which is connected to a body ...
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WO/2021/012471A1 |
The present invention relates to an electric aviation catering vehicle upward loading driving method. There are three driving modes: 1. a normal working mode, wherein a high-voltage power battery drives an upward loading oil pump to work...
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WO/2021/009464A1 |
Tool (100) for disassembling and moving a TRV-type turbine casing (24) from an aircraft turbine engine (10), said turbine casing comprising two annular shrouds, inner (24a) and outer (24b) shrouds respectively, which extend one inside th...
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